The Role of Modeling and Flight Testing in Rotorcraft Parameter Identification
Author | : R. T. N. Chen |
Publisher | : |
Total Pages | : 46 |
Release | : 1986 |
ISBN-10 | : CORNELL:31924051598294 |
ISBN-13 | : |
Rating | : 4/5 (94 Downloads) |
Book excerpt: The importance of recognizing that each lower-order model used for rotorcraft parameter identification has a limited range of applicability is illustrated in some detail. Examples are given to illustrate the use of conditioning the test input signals and the potential of using multi-axis test inputs to enhance the parameter identifiability. The paper discusses the benefits and limitations of using frequency sweeps as flight-test input signals for identification of frequency response for rotorcraft and for the subsequent fitting of parametric transfer-function models. This paper demonstrates the major role played by analytical modeling and the understanding of the physics involved in the rotorcraft flight dynamics, particularly understanding the limit of lower-order models, in achieving successful rotorcraft parameter identification. (Author).